Numerical investigation of transverse jets through multiport injector arrays in a supersonic crossflow AS Pudsey, RR Boyce Journal of Propulsion and Power 26 (6), 1225-1236, 2010 | 121 | 2010 |
Behavior of multiple-jet interactions in a hypersonic boundary layer AS Pudsey, V Wheatley, RR Boyce Journal of Propulsion and Power 31 (1), 144-155, 2015 | 64 | 2015 |
Hypersonic viscous drag reduction via multiporthole injector arrays AS Pudsey, RR Boyce, V Wheatley Journal of Propulsion and Power 29 (5), 1087-1096, 2013 | 54 | 2013 |
Influence of common modeling choices for high-speed transverse jet-interaction simulations AS Pudsey, RR Boyce, V Wheatley Journal of Propulsion and Power 29 (5), 1076-1086, 2013 | 41 | 2013 |
Numerical investigation of upstream cavity enhanced fuel mixing in scramjet combustors T Roos, A Pudsey, M Bricalli, H Ogawa Acta Astronautica 169, 50-65, 2020 | 33 | 2020 |
Cavity enhanced jet interactions in a scramjet combustor T Roos, A Pudsey, M Bricalli, H Ogawa Acta Astronautica 157, 162-179, 2019 | 26 | 2019 |
Supersonic boundary-layer combustion via multiporthole injector arrays AS Pudsey, V Wheatley, RR Boyce AIAA Journal 53 (10), 2890-2906, 2015 | 23 | 2015 |
Scramjet performance with nonuniform flow and swept nozzles MG Bricalli, L Brown, RR Boyce, R Gollan, T Vanyai, AS Pudsey AIAA Journal 56 (10), 3988-4003, 2018 | 14 | 2018 |
Numerical investigation of combustion characteristics of upstream crescent cavities in a scramjet combustor T Roos, A Pudsey, H Ogawa Acta Astronautica 187, 43-60, 2021 | 12 | 2021 |
Numerical investigation of fuel mixing with upstream crescent cavities in a scramjet combustor T Roos, A Pudsey, M Bricalli, H Ogawa Acta Astronautica 177, 611-626, 2020 | 12 | 2020 |
Mixing characteristics of cracked gaseous hydrocarbon fuels in a scramjet combustor M Ravindran, M Bricalli, A Pudsey, H Ogawa Acta Astronautica 162, 168-184, 2019 | 12 | 2019 |
Full flow-path optimization of axisymmetric scramjet engines H Ogawa, Y Alazet, A Pudsey, R Boyce, A Isaacs, T Ray 17th AIAA International Space Planes and Hypersonic Systems and Technologies …, 2011 | 10 | 2011 |
SCRAMSPACE: Radical-Farming Scramjet for access to space S Tirtey, R Boyce, M Brown, B Capra, M Creagh, A Dedman, I Dimitrijevic, ... Hypersonic Flight Testing, 1-31, 2014 | 7 | 2014 |
Mixing enhancement in a hydrocarbon-fuelled scramjet engine through repeated laser sparks F Rogg, M Bricalli, S O'Byrne, AS Pudsey, P Marzocca 23rd AIAA International Space Planes and Hypersonic Systems and Technologies …, 2020 | 5 | 2020 |
Analysis of a multi-porthole injector array in a supersonic crossflow MG Bricalli, M Pfeiffer, AS Pudsey, K Basore Journal of Propulsion and Power 36 (4), 560-574, 2020 | 4 | 2020 |
Impact of Life Cycle Assessment Considerations on Launch Vehicle Design T Bellier, A Urbano, J Morlier, C Bil, A Pudsey 73rd International Astronautical Congress (IAC) 2022–Paris, France, 2022 | 3 | 2022 |
Laser-induced fluorescence investigations for temperature measurements in a carbon dioxide flow M Kirschner, AS Pudsey, F Koroll, T Sander, C Mundt Journal of Thermophysics and Heat Transfer 32 (1), 216-225, 2018 | 3 | 2018 |
Heat flux measurements of a methane-oxygen rotating detonation rocket engine R Aliakbari, Q Michalski, N Mason-Smith, A Pudsey, M Wenzel, N Paull International Workshop on Detonation Propulsion, 2022 | 2 | 2022 |
Numerical investigation of upstream cavity enhanced combustion in a scramjet combustor T Roos, AS Pudsey, M Bricalli, H Ogawa 23rd AIAA International Space Planes and Hypersonic Systems and Technologies …, 2020 | 2 | 2020 |
Numerical simulations of radiative heat effects in a plasma wind-tunnel flow under Mars entry conditions J García-Garrido, AS Pudsey, C Mundt Acta Astronautica 151, 334-341, 2018 | 2 | 2018 |